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You searched for: (collection:ufnaca OR mediatype:ufnaca) AND -mediatype:collection AND firstTitle:T
[texts]Tables and charts for the evaluation of profile drag from wake surveys at high subsonic speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003616157&ix=nu&I=0&V=D&pm=1
Keywords: Wakes (Aerodynamics; Aerodynamics--Research
Downloads: 133
[texts]Temperature recovery factors on a slender 12° cone-cylinder at Mach numbers from 3.0 to 6.3 and angles of attack up to 45° - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854733&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Laminar boundary layer--Research; Aerodynamics--Research
Downloads: 96
[texts]Tensile tests of NACA and conventional machine-countersunk flush rivets - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807455&ix=nu&I=0&V=D&pm=1
Keywords: Rivets and riveting, Aircraft; Aerodynamics--Research
Downloads: 171
[texts]Tests of a linked differential flap system designed to minimize the reduction in effective dihedral caused by power - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003631486&ix=nu&I=0&V=D&pm=1
Keywords: Flaps (Airplanes; Aerodynamics--Research
Downloads: 86
[texts]Tests of a stress-carrying door in compression - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806501&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 85
[texts]Tests of a stress-carrying door in shear - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003806509&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Design and construction; Aerodynamics--Research
Downloads: 116
[texts]Theoretical analysis of stationary potential flows and boundary layers at high speed =: Theoretische untersuchungen über stationäre potentialströmungen und grenzschichten bei hohen geschwindigkeiten - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003604221&ix=nu&I=0&V=D&pm=1
Keywords: Gas dynamics; Laminar boundary layer; Aerodynamics--Research
Downloads: 80
[texts]Theoretical and experimental dynamic loads for a prismatic float having an angle of dead rise of 22 1/2° - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638573&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes--Hydrodynamics; Aerodynamics--Research
Downloads: 94
[texts]Theoretical and experimental investigation of arbitrary aspect ratio, supercavitating hydrofoils operating near the free water surface - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834456&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 142
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 86
[texts]Theoretical distribution of load over a swept-back wing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003805176&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Swept-back; Vortex theory (Astrophysics; Aerodynamics--Research
Downloads: 109
[texts]Theoretical investigation of drag reduction in maintaining the laminar boundary layer by suction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780451&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Laminar boundary layer
Downloads: 179
[texts]Theoretical investigation of the drag of generalized aircraft configurations in supersonic flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874442&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerodynamics, Supersonic; Airplanes--Design and construction
Downloads: 113
[texts]Theories of turbulence - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807732&ix=nu&I=0&V=D&pm=1
Keywords: Turbulence; Aerodynamics--Research
Downloads: 159
[texts]Theory of propellers.: II,Method for calculating the axial interference velocity - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807489&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 151
[texts]Theory of propellers.: III, the slipstream contraction with numerical values for two-blade and four-blade propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003638511&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 186
[texts]Theory of propellers.:I, Determination of the circulation function and the mass coefficient for dual-rotating propellers - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003622107&ix=nu&I=0&V=D&pm=1
Keywords: Propellers, Aerial; Aerodynamics--Research
Downloads: 140
[texts]Tire friction coefficients and their relation to ground-run distance in landing - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808568&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Tires--Traction; Aerodynamics--Research
Downloads: 220
[texts]Transition caused by the Laminar flow separation - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778661&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Laminar flow; Boundary layer
Downloads: 75
[texts]Turbulence in the wake of a thin airfoil at low speeds - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875247&ix=nu&I=0&V=D&pm=1
Keywords: Downwash (Aerodynamics; Airplanes--Wings--Testing
Downloads: 233
[texts]Two-dimensional motion of a gas at large supersonic velocities - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003690375&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics, Supersonic; Mach number
Downloads: 97
[texts]Two-dimensional potential flows : = Ebene potentialströmungen - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003690307&ix=nu&I=0&V=D&pm=1
Keywords: Differential equations; Speed; Aeronautics
Downloads: 83
[texts]Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 651-210 airfoil section - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003600239&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics--Research
Downloads: 83
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